Pratt & Whitney Canada PW308A
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Dassault_Falcon_2000DX
gptkb:Dassault_Falcon_2000EX gptkb:Dassault_Falcon_2000S gptkb:Dassault_Falcon_2000LX |
| gptkbp:bypassRatio |
4.3:1
|
| gptkbp:certification |
1997
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:cycle |
two-spool
|
| gptkbp:diameter |
34.5 in
|
| gptkbp:family |
gptkb:PW300
|
| gptkbp:firstRun |
1995
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PW308A
|
| gptkbp:length |
72.6 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfStages |
2
1 fan, 2 axial, 1 centrifugal |
| gptkbp:thrust |
6,900 lbf
|
| gptkbp:weight |
1,625 lb
|
| gptkbp:bfsParent |
gptkb:Beechcraft_Model_4000
|
| gptkbp:bfsLayer |
6
|